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- W68856828 abstract "The use of various finite elements (FE) for the analysis of reinforced-shell aerospace structures is discussed in this paper. One-, two-, and three-dimensional FE models from a commercial code are compared to higher-order beam theories, which are implemented by using the Carrera Unified Formulation (CUF). CUF is a hierarchical formulation allowing for the straightforward implementation of any order-beam theories without the need of ad-hoc formulations. The attention is here focused on a novel approach denoted as Component-Wise (CW). According to CUF, Lagrange-like polynomials are used in CW models to discretize the displacement field on the cross-section of each component of the structure. Depending on the geometrical and material characteristics of the component, the capabilities of the model can be enhanced and the computational costs can be kept low through smart discretization strategies. The global mathematical model of complex structures (e.g. wings or fuselages) is obtained by assembling each component model at the cross-section level. Next, a classical 1D FE formulation is used to develop numerical applications. A number of typical aerospace structures are analysed. Static and dynamic analyses highlight the enhanced capabilities of the proposed formulation. In fact, the CW approach is clearly the natural tool to analyse aerospace structures, since it leads to results that can be only obtained through threedimensional elasticity (solid) elements whose computational costs are at least one-order of magnitude higher than CW models." @default.
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- W68856828 date "2013-01-01" @default.
- W68856828 modified "2023-09-27" @default.
- W68856828 title "Effect of loading factors on the Analysis of Aeronautical Structures by Component-Wise Models" @default.
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